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FREE-FLIGHT INVESTIGATION AT SUPERSONIC SPEEDS OF THE STABILITY AND DRAG OF A 79 DEG CLIPPED DELTA BOOST-GLIDE CONFIGURATION INCLUDING AN ANALOG STUDY OF COUPLED MOTIONS DURING THE FLIGHTSupersonic free-flight test of delta boost-glide figure with analog study of coupled motions
Document ID
19630004031
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blanchard, W. S., Jr. (NASA Langley Research Center Hampton, VA, United States)
Hoffman, S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1961
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-425
Report Number: NASA-TM-X-425
Accession Number
63N13907
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FREE FLIGHT
AERODYNAMIC CHARACTERISTICS
DELTA WING
BOOST GLIDE
SUPERSONIC SPEED

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